View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 27843U 26145.47310815 +.00000000 +00000-0 +49525-4 0 00003
2 27843 98.7048 153.5161 0009111 323.7450 36.3109 14.21317046 01
| Epoch (UTC): | 25 May 2026 11:21:16 |
| Eccentricity: | 0.0009111 |
| inclination: | 98.7048° |
| perigee height: | 814 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 153.5161° |
| argument of perigee: | 323.7450° |
| revolutions per day: | 14.21317046 |
| mean anomaly at epoch: | 36.3109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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